idrag input file asample2 - an elliptic load distribution 1 input mode 1 write flag 1 symmetry flag 1 load flag 0. x cg position 0.25 center of pressure for airfoil sections 0.15 reference area 0.15 reference chord 1 number of panels 0 0 0 x,y,z for 4 corners of panel 1 0 0.5 0 0.2 0.5 0 0.2 0 0 10 number of vortices for panel 1 0 vortex spacing for panel 1 11 number of loads for panel 1 0.0000 1.0000 load station 1, load 1, for panel 1 0.1000 0.9950 load station 2, load 2, for panel 1 0.2000 0.9798 load station 3, load 3, for panel 1 0.3000 0.9539 load station 4, load 4, for panel 1 0.4000 0.9165 load station 5, load 5, for panel 1 0.5000 0.8660 load station 6, load 6, for panel 1 0.6000 0.8000 load station 7, load 7, for panel 1 0.7000 0.7141 load station 8, load 8, for panel 1 0.8000 0.6000 load station 9, load 9, for panel 1 0.9000 0.4359 load station 10, load 10, for panel 1 1.0000 0.0000 load station 11, load 11, for panel 1